Entry guidance with real-time planning of reference based on analytical solutions

Author:

Yu Wenbin,Chen Wanchun

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference29 articles.

1. A Common Aero Vehicle (CAV) Model, Description, and Employment Guide;Phillips,2003

2. Harpold, J.C., Graves, C.A., 1979. Shuttle entry guidance, NASA Lyndon B. Johnson Space Center, Houston, TX. Rep. JSC-14694.

3. Hanson, J.M., Coughlin, D.J., et al., 1998. Ascent, transition, entry, and abort guidance algorithm design for the X-33 vehicle. In: AIAA Paper 98-4409.

4. Reduced-order entry trajectory planning for acceleration guidance;Mease;J. Guid. Control Dyn.,2002

5. Dukeman, G.A., 2002. Profile-following entry guidance using linear quadratic regulator theory. In: AIAA Paper 2002-4457.

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